AIRCRAFT SHOCK STRUT HAVING IMPROVED CYLINDER AND BEARINGS
摘要
An aircraft shock strut (12) includes a titanium cylinder (32) and a piston (30) telescopically movable within the titanium cylinder (32). A first bearing (40) is mounted to the piston (30), and includes a non-metallic bearing surface (50) for providing sliding engagement with the titanium cylinder (32). The aircraft shock strut (12) provides weight savings along with durability.
申请公布号
WO2008048335(A3)
申请公布日期
2008.08.14
申请号
WO2007US00904
申请日期
2007.01.12
申请人
GOODRICH CORPORATION;LUCE, WILLIAM, E.;MAITLAND, SCOTT